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JPS5945878B2 - cryostat - Google Patents
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JPS5945878B2 - cryostat - Google Patents

cryostat

Info

Publication number
JPS5945878B2
JPS5945878B2 JP53043679A JP4367978A JPS5945878B2 JP S5945878 B2 JPS5945878 B2 JP S5945878B2 JP 53043679 A JP53043679 A JP 53043679A JP 4367978 A JP4367978 A JP 4367978A JP S5945878 B2 JPS5945878 B2 JP S5945878B2
Authority
JP
Japan
Prior art keywords
inner tank
cryostat
gas
shield plate
radiation shield
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP53043679A
Other languages
Japanese (ja)
Other versions
JPS54136415A (en
Inventor
昭徳 尾原
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP53043679A priority Critical patent/JPS5945878B2/en
Publication of JPS54136415A publication Critical patent/JPS54136415A/en
Publication of JPS5945878B2 publication Critical patent/JPS5945878B2/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C3/00Vessels not under pressure
    • F17C3/02Vessels not under pressure with provision for thermal insulation
    • F17C3/08Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
    • F17C3/085Cryostats
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2221/00Handled fluid, in particular type of fluid
    • F17C2221/01Pure fluids
    • F17C2221/014Nitrogen
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F17STORING OR DISTRIBUTING GASES OR LIQUIDS
    • F17CVESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
    • F17C2270/00Applications
    • F17C2270/05Applications for industrial use
    • F17C2270/0509"Dewar" vessels

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
  • Containers, Films, And Cooling For Superconductive Devices (AREA)

Description

【発明の詳細な説明】 この発明はクライオスタット(超低温用容器)の改良に
関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an improvement in a cryostat (an ultra-low temperature container).

第1図は従来のクライオスタット(ヘリウム用クライオ
スタット)の断面構成を示す図で、図中1は外槽、21
、22はアルミ蒸着マイラ等を反射材、ガラスペーパー
等をスペーサとして数拾層積ねてなる多層断熱材で、断
熱真空部を形成している。
Figure 1 is a diagram showing the cross-sectional configuration of a conventional cryostat (helium cryostat), in which 1 is an outer tank, 21
, 22 is a multilayer heat insulating material made by laminating several layers of aluminum vapor-deposited mylar or the like as a reflective material and glass paper or the like as a spacer, forming an insulating vacuum section.

3は外槽1の内側に上記多層断熱材2、を介して設けら
れた輻射シールド板、4は冷却管、5は上記輻射シール
ド板3で囲まれた部分の内方に形成された内槽、6はこ
の内槽5に収納された超電導コイル、7は内槽5内に貯
蔵された液体ヘリウム、8は弁である。
3 is a radiation shield plate provided inside the outer tank 1 via the multilayer insulation material 2, 4 is a cooling pipe, and 5 is an inner tank formed inside the part surrounded by the radiation shield plate 3. , 6 is a superconducting coil housed in the inner tank 5, 7 is liquid helium stored in the inner tank 5, and 8 is a valve.

点a、bおよびcはそれぞれ温度測定点を指すもので、
点aは内槽壁、点bは輻射シールド板3と内槽5との間
の多層断熱材22中心部、点cは輻射シールド板3の各
部を指す。第2図はこれらの温度測定点a−cにおける
温度変化の状態を示すグラフで、図中a−cは上記温度
測定点a−cに対応する・ところで、一般にヘリウム用
クライオスタットの運転においては、内槽5を常温(3
00゜に)から液体ヘリウム温度(4.2゜に)に冷却
した後、内槽5に必要レベルまで液体ヘリウムTを貯蔵
する。
Points a, b and c each indicate temperature measurement points,
Point a indicates the inner tank wall, point b indicates the center of the multilayer insulation material 22 between the radiation shield plate 3 and the inner tank 5, and point c indicates each part of the radiation shield plate 3. Figure 2 is a graph showing the state of temperature change at these temperature measurement points a-c, in which a-c corresponds to the temperature measurement points a-c mentioned above.By the way, in general, in the operation of a helium cryostat, Keep the inner tank 5 at room temperature (3
After cooling from 00°) to liquid helium temperature (4.2°), liquid helium T is stored in the inner tank 5 to the required level.

しかしながら上述従来のクライオスタットは、輻射シー
ルド板3と内槽5との間が断熱真空状態であるため、こ
の部分の多層断熱材22の中心部(点b)の稠度平衡が
第2図に示すよう長時間を要する。このため安定状態で
行う必要のあるクライオスタットの熱的特性の測定、あ
るいは内部に収納した超電導コイル6等の静特性の測定
において長い待ち時間を必要とする等の欠点があつた。
この発明は上記のような欠点を除去するためになされた
もので、温度平衡時間を短縮したクライオスタットを提
供することを目的とする。以下第3図および第4図を参
照してこの発明の実施例を説明する。
However, in the conventional cryostat described above, since the space between the radiation shield plate 3 and the inner tank 5 is in an adiabatic vacuum state, the consistency balance at the center (point b) of the multilayer insulation material 22 in this area is as shown in FIG. It takes a long time. For this reason, there were drawbacks such as a long waiting time being required when measuring the thermal characteristics of the cryostat, which must be carried out in a stable state, or when measuring the static characteristics of the superconducting coil 6 etc. housed inside.
This invention was made to eliminate the above-mentioned drawbacks, and an object thereof is to provide a cryostat with a shortened temperature equilibration time. Embodiments of the present invention will be described below with reference to FIGS. 3 and 4.

第3図はこの発明によるクライオスタットの一実施例を
示す断面構成図で、図中1〜8および点a−cはそれぞ
れ第1図と同様であり、、説明の重複を避けるために同
様の部分に同一符号を付した。9は輻射シールド板3と
内槽5との空間、換言すれば多層断熱材22を有する部
分に封じ込まれた窒素ガス、10はその封切弁である。
FIG. 3 is a cross-sectional configuration diagram showing one embodiment of the cryostat according to the present invention, in which points 1 to 8 and points a to c are the same as in FIG. 1, and similar parts are shown to avoid duplication of explanation. are given the same reference numerals. Reference numeral 9 indicates nitrogen gas sealed in the space between the radiation shield plate 3 and the inner tank 5, in other words, the portion having the multilayer insulation material 22, and 10 indicates a shutoff valve thereof.

第4図は第2図と同様に温度測定点a〜cにおける温度
変化の状態を示すグラフである。すなわちこの発明は、
内槽5に貯蔵する液化ガス、ここでは液体ヘリウム7よ
り沸点の高いガスここでは窒素ガス9を輻射シールド板
3と内槽5との空間内に封じ込んだものである。このよ
うなクライオスタツトにおいて、いま、その冷却は従米
のクライォスタツトと同じ方法で行うものとすれば、内
槽5の温度が3000K〜約500Kの範囲では、輻射
シールド板3と内槽5との間の多層断熱材22の中心部
の点b(7)温度はその空間に封じ込められた窒素ガス
9の伝導、対流作用によつて容易に冷やされ、第4図に
示すように短時間でも500K程度になる。
Similar to FIG. 2, FIG. 4 is a graph showing the state of temperature change at temperature measurement points a to c. In other words, this invention
A liquefied gas stored in the inner tank 5, here a gas having a higher boiling point than liquid helium 7, here nitrogen gas 9, is sealed in the space between the radiation shield plate 3 and the inner tank 5. In such a cryostat, if cooling is performed in the same manner as in American cryostats, when the temperature of the inner tank 5 is in the range of 3000K to about 500K, the gap between the radiation shield plate 3 and the inner tank 5 is The temperature at point b (7) at the center of the multilayer insulation material 22 is easily cooled down by conduction and convection of the nitrogen gas 9 confined in that space, and as shown in Fig. 4, the temperature at point b (7) is about 500 K even for a short time. become.

その後、内槽5の湛度が400K以下に下がれば、上記
空間の窒素ガス9はクライオポンプの作用によつて内槽
壁に固化吸着されてしまい、空間は1×101T0rr
以下の真空になる。このため従来のクライオと同等の断
熱効果を得ることができ、何ら弊害なく各部の渦度平衡
時間力吠きく短縮される(第4図参照)。なお、上述実
施例では内槽5に貯蔵する液化ガスが液体ヘリウム7で
、ヘリウム用クライオスタツトを例示し、封じ込むガス
を窒素ガス9として説明したが、これのみに限られず、
液化ガスが例えば液体水素、液体アルゴンで、封じ込む
ガスがこれらの液化ガスよリ沸点が高いガスであればア
ルゴン、酸素等であつてもこの発明を適用できることは
いうまでもない。
After that, when the filling degree of the inner tank 5 falls below 400K, the nitrogen gas 9 in the space is solidified and adsorbed to the inner tank wall by the action of the cryopump, and the space becomes 1×101T0rr.
The vacuum becomes below. Therefore, it is possible to obtain a heat insulation effect equivalent to that of the conventional cryo, and the vorticity equilibrium time of each part is significantly shortened without any adverse effects (see Fig. 4). In the above embodiment, the liquefied gas stored in the inner tank 5 is liquid helium 7, the cryostat for helium is illustrated, and the gas to be sealed is nitrogen gas 9, but the present invention is not limited to this.
It goes without saying that the present invention can be applied to argon, oxygen, etc. as long as the liquefied gas is, for example, liquid hydrogen or liquid argon, and the gas to be enclosed has a higher boiling point than these liquefied gases.

以上述べたようにこの発明によれば、内槽5に貯蔵する
液化ガスより沸点の高いガスを輻射シールド板3と内槽
5との空間内に封じ込んだので温度平衡時間を大きく短
縮することができる。
As described above, according to the present invention, since the gas having a higher boiling point than the liquefied gas stored in the inner tank 5 is sealed in the space between the radiation shield plate 3 and the inner tank 5, the temperature equilibrium time can be greatly shortened. Can be done.

従つてクライオスタツトの熱的特性の測定、あるいは内
部に収納した超電導コイル6等の静特性の測定における
待ち時間も大きく短縮することができるという効果があ
る。
Therefore, there is an effect that the waiting time for measuring the thermal characteristics of the cryostat or the static characteristics of the superconducting coil 6 etc. housed inside can be greatly shortened.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は従来のクライオスタツトの断面構成図第2図は
同上クライオスタット各部における混度変化の状態を示
すグラフ、第3図はこの発明によるクライオスタツトの
一実施例を示す断面構成図、第4図は同上クライオスタ
ット各部における温度変化の状態を示すグラフである。 1・・・・・・外槽、21,22・・・・・・多層断熱
材、3・・・輻射シールド板、5・・・・・・内槽、7
・・・・・・液体ヘリウム(液化ガス)9・・・・・・
窒素ガス(液化ガスよリ沸点の高いガス)。
FIG. 1 is a cross-sectional configuration diagram of a conventional cryostat. FIG. 2 is a graph showing the state of mixture change in each part of the same cryostat. FIG. 3 is a cross-sectional configuration diagram showing an embodiment of the cryostat according to the present invention. The figure is a graph showing the state of temperature change in each part of the same cryostat. 1...Outer tank, 21, 22...Multilayer insulation material, 3...Radiation shield plate, 5...Inner tank, 7
・・・・・・Liquid helium (liquefied gas) 9・・・・・・
Nitrogen gas (a gas with a higher boiling point than liquefied gas).

Claims (1)

【特許請求の範囲】 1 外槽と、この外槽の内槽に断熱真空部を介して設け
られた輻射シールド板と、この輻射シールド板で囲まれ
た部分の内方に形成された内槽と、上記輻射シールド板
と内槽との空間に設けられた多層断熱材とからなるクラ
イオスタットにおいて、内槽に貯蔵する液化ガスより沸
点の高いガスを上記空間内に封じ込んだことを特徴とす
るクライオスタット。 2 内槽に貯蔵する液化ガスがヘリウムガスであり、上
記空間内に封じ込むガスが窒素ガスである特許請求の範
囲第1項記載のクライオスタット。
[Scope of Claims] 1. An outer tank, a radiation shield plate provided to the inner tank of the outer tank via an insulating vacuum section, and an inner tank formed inside the area surrounded by the radiation shield plate. and a multilayer insulation material provided in a space between the radiation shield plate and the inner tank, characterized in that a gas having a higher boiling point than the liquefied gas stored in the inner tank is sealed in the space. Cryostat. 2. The cryostat according to claim 1, wherein the liquefied gas stored in the inner tank is helium gas, and the gas sealed in the space is nitrogen gas.
JP53043679A 1978-04-13 1978-04-13 cryostat Expired JPS5945878B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP53043679A JPS5945878B2 (en) 1978-04-13 1978-04-13 cryostat

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP53043679A JPS5945878B2 (en) 1978-04-13 1978-04-13 cryostat

Publications (2)

Publication Number Publication Date
JPS54136415A JPS54136415A (en) 1979-10-23
JPS5945878B2 true JPS5945878B2 (en) 1984-11-09

Family

ID=12670517

Family Applications (1)

Application Number Title Priority Date Filing Date
JP53043679A Expired JPS5945878B2 (en) 1978-04-13 1978-04-13 cryostat

Country Status (1)

Country Link
JP (1) JPS5945878B2 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS59157200U (en) * 1983-04-08 1984-10-22 三菱電機株式会社 cryogenic container
JPS59172900U (en) * 1983-05-07 1984-11-19 三菱電機株式会社 cryogenic container
JPS60147000A (en) * 1984-01-11 1985-08-02 Mitsubishi Electric Corp Cryogenic container
CN100357454C (en) * 2005-07-01 2007-12-26 本溪冶炼集团有限公司 Ferro-aluminium alloy with low carbon, low phosphor and low sulphur content for final deoxidizer in steelmaking
JP6619551B2 (en) * 2014-09-30 2019-12-11 川崎重工業株式会社 Dual structure tube for cryogenic fluid and dual structure storage tank for cryogenic fluid

Also Published As

Publication number Publication date
JPS54136415A (en) 1979-10-23

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